CN105115358A - Rotational centrifugal launcher - Google Patents
Rotational centrifugal launcher Download PDFInfo
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- CN105115358A CN105115358A CN201510522916.8A CN201510522916A CN105115358A CN 105115358 A CN105115358 A CN 105115358A CN 201510522916 A CN201510522916 A CN 201510522916A CN 105115358 A CN105115358 A CN 105115358A
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- launching
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Abstract
The invention discloses a rotational centrifugal launcher which comprises a power device, a control device, an accelerator and a base. The power device is composed of a driving motor (1) and a speed changing mechanism (15); the control device (3) adopts a single chip microcomputer or a computer to control the speed changing mechanism (15) and the launching initial speeds and launching angles of launching objects (4); the accelerator comprises a rotating device (5), multiple launching canisters (16) and electromagnetic releasing mechanisms (7), the launching canisters (16) are fixed on the edge of the whole circumference of the rotating device (5) and driven by the power device to rotate to reach certain revolutions, and therefore the launching objects (4) in the launching canisters (16) can acquire certain initial speed and kinetic energy. The rotational centrifugal launcher is small in size and weight and high in invisibility and launching precision, one launcher can launch warheads of different warhead diameters, and single launching, continuous launching and mass launching can be all achieved; heavy objects can be safely sent to the far place at low cost, even the outer space.
Description
Technical field
The present invention relates to a kind of centrifugal device, especially relate to the device utilizing centrifugal force to be projected away by weight, for the field such as weaponry and space lunch.
Background technology
By object or weight, launch with certain initial velocity, such as emission bullet or shell, and space ship transmitting is entered space track, the method adopted at present promotes object injection by chemical fuel burning acquisition kinetic energy; But in chemical fuel combustion process, can discharge a large amount of heat energy and sound, energy loss is large, and the conversion efficiency of these fuel is not high substantially.
The initial velocity that general bullet goes out thorax is 300 meters per second, speed when shell goes out thorax depends on the draw ratio of bore and gun tube, gunpowder needs one period of acceleration time to shell, and the longer initial velocity of gun barrel generally with bore is higher, and certain barrel is long also has the limit.Different cannon initial velocity is also different, and gun is generally at 1300 meter per second-1900 meter per seconds, and howitzer is generally at 900 meter per second-1500 meter per seconds.With the type smooth bore big gun initial velocity of cannon also higher than rifle cannon, as tank gun is all its initial velocity of smooth bore big gun mostly all about 1900 meter per seconds.And the initial velocity of mortar is relatively just much lower general about 100 meter per second-300 meter per seconds.
In order to reach the cannon initial velocity of 1900 meter per seconds, the length of gun tube and the ratio of gun barrel diameter have reached 52 times, continue to improve initial velocity, add Long Barrel, for the manufacture of artillery brings difficulty.
In order to overcome many disadvantages of above-mentioned chemical gunpowder, current progress is the principle adopting Electromagnetic Drive, such as, adopt magnetic artillery, the devices such as electromagnetic launch.
The principle of magnetic artillery is very simple, and in 19th century, British scientist faraday finds, the wire being arranged in magnetic field can be subject to the promotion of a power when being energized, meanwhile, if allow wire do the motion of cutting magnetic line in magnetic field, and also can generation current on wire.Famous Faraday's electromagnetic induction law that Here it is.Generator and the motor of present extensive use has been invented just according to this law people, it is also the general principle of magnetic artillery, and in other words, magnetic artillery is only a kind of more special motor, because its rotor is not rotate, but makes the shell of linear accelerating motion.So how to produce the magnetic field driving shell, and allow electric current through shell, make it obtain the power advanced? a magnetic artillery design the simplest is as follows:
Make track with two conductors, middle placement shell, makes electric current can set up loop by three.This device is placed in magnetic field, and to shell energising, shell will accelerate to fly out forward.The shell that it is 300 grams quality has accelerated to about 4 kms per second.If in a vacuum, this speed also can bring up to 8 ~ 10 kms per second, and this has exceeded the first universal speed, has possessed the theoretical qualification as a kind of novel space launch device.In order to this theoreticly may be become reality, also need to solve following problem:
First, as airship, the acceleration of calutron can not be too large, otherwise people cannot bear.Solution extends the acceleration time.But this must to adopt longer track for cost.Because human body can only bear the long-time acceleration of about 3 times of acceleration of gravity, for reaching the first universal speed, as calculated, the track length needed for calutron meeting Human Tolerance ability about needs 1000 kms, and this is difficult to realize technically.
The second, the shell quality that current magnetic artillery can be launched is still little, and this is that acceleration capacity deficiency causes.The power accelerating shell is directly proportional to magnetic field and the amassing of electric current, obtain enough strong acceleration magnetic field, in general by superconducting magnet.The technology that magnetic field has been relative maturity is produced with superconducting coil. but superconducting magnet needs to be cooled to very low temperature, competence exertion effect, as liquid helium temperature about-269 DEG C, this is a problem for Military Application, because the flexibility of emitter greatly can be reduced, actual battlefield can not be used in.
Finally, someone feels to build kilometer level length, and the technical difficulty that the acceleration orbit being equipped with high-intensity magnetic field may run into also comprises the required precision of circuit construction high, and the places such as each turning and control point also all need to arrange high-intensity magnetic field.
As for the launch cost of magnetic artillery, except powerful electrical source consumption, also will consider the super-low liquid expense producing high-intensity magnetic field, cost is relatively high.
Summary of the invention
The object of the invention is to overcome the deficiencies in the prior art, propose a kind of rotating centrifugal transmitter, this device can with lower cost, makes object reach impelling go out required initial velocity by CENTRIFUGAL ACCELERATING device.
Technical solution of the present invention is:
A kind of rotating centrifugal transmitter, it is characterized in that, described rotating centrifugal transmitter comprises: power set, control device, accelerator and base;
Described power set are made up of drive motors 1 and gear 15, and drive motors 1 adopts ac motor or the dc motor of different capacity and rotating speed;
Control device 3 adopts single-chip microcomputer or computer, controls the initial velocity of the transmitting of speed change gear 15 and emitting substance 4 and emission angle;
Described accelerator comprises whirligig 5, multiple launching tube 16 and electromagnetic release unit 7, described launching tube 16 is fixed on the edge of the whole circumference of described whirligig 5, described whirligig 5 drives rotation to reach certain revolution by power set, makes the emitting substance 4 in launching tube 16 obtain certain initial velocity and kinetic energy;
Described base 2 supports whole device, providing stable and guide effect, improving fire accuracy for launching.
The length of described launching tube 16 is corresponding with the length of emitting substance 4, arranges rifling in launching tube 16.
Described speed change gear 15 adopts mechanical variable speed device or variable-frequency governor, makes whirligig 5 reach predetermined number of revolutions.
Described mechanical variable speed device is speed-changing gear box.
Described drive unit is rocking handle 6.
Described electromagnetic release unit 7, according to the arranged of launching tube 16, is arranged on the afterbody of each launching tube 16, utilizes wire 8 to be connected with control device 3 by each electromagnetic release unit 7.
Described electromagnetic release unit 7 comprises electromagnet, brute spring 12 and friction plate 9, wherein, the iron core 10 of electromagnet is hollow form, arrange coil 11 in described iron core 10, the spatial placement brute spring 12 in iron core 10, described brute spring 12 is stage clip, between electromagnet end cap 13 and electromagnet armature 14, the another side riveted joint friction plate 9 of described armature 14.
Beneficial effect of the present invention:
Rotating centrifugal transmitter of the present invention can low cost, and being sent away by weight of safety, even enters space.
For firing shells, length and the initial velocity of gun barrel have nothing to do, and the moment of launching, can reach the initial velocity of 1900 meter per seconds, need not by lengthening the length of gun barrel; For the rifle cannon only demand fulfillment gun barrel with the rifling of certain length that makes shell rotate; For smooth bore big gun, the length only demand fulfillment shell length of gun barrel.
For space lunch, because the increase of rotating speed can be controlled, in the scope of the acceleration of the 2-3g that acceleration can bear people, the acceleration of gravity born is low.
Launch cost is low, is only power consumption; Volume is little, mobility strong; Regular maintenance cost is low, is only the maintenance of general motor and mechanical driving device.
Accompanying drawing explanation
Fig. 1 is rotating centrifugal emitter structures schematic diagram of the present invention;
Fig. 2 shows hand grenade instrumentation structural representation;
Fig. 3 shows electromagnetic release device arrangement architecture;
Fig. 4 is electromagnetic release device structural representation.
1 motor 9 friction plate
2 base 10 iron cores
3 control device 11 coils
4 emitting substance 12 brute springs
5 whirligig 13 end caps
6 rocking handle 14 armature
7 electromagnetic release unit 15 speed change gears
8 wire 16 launching tubes
Detailed description of the invention
Below in conjunction with accompanying drawing, method of the present invention is described in detail.
Fig. 1 is rotating centrifugal emitter structures schematic diagram of the present invention; As shown in the figure, rotating centrifugal transmitter comprises: power set, control device, accelerator and base.
Power set are made up of drive motors 1 and gear 15, and drive motors 1 can adopt ac motor or dc motor, according to the needs of launch mission, select the motor of different capacity and rotating speed;
Control device 3 adopts single-chip microcomputer or computer.The transmitting of speed change gear 15 and emitting substance 4 is controlled, comprises the initial velocity of transmitting and the control of emission angle;
Accelerator comprises whirligig 5, launching tube 16 and electromagnetic release unit 7, multiple launching tubes 16 are fixed on the edge of the whole circumference of whirligig 5, drive whirligig 5 to rotate by motor 1 and speed change gear 15 and reach certain revolution, make the emitting substance 4 in launching tube 16 obtain certain initial velocity, thus obtain kinetic energy;
Base 2 supports whole device, providing stable and guide effect, improving fire accuracy for launching.
Launching tube 16 is different with conventional gun barrel, do not need to lengthen the effect of shell to extend gunpowder, it has been only the effect of auto levelizer emitting substance 4, or, if in order to arrange rifling in launching tube, emitting substance being rotated, playing guiding, stabilization, also only need to run limited distance in launching tube, therefore also greatly shorten than conventional paulownia.
Speed change gear 15 can adopt mechanical variable speed device, as speed-changing gear box, also can adopt variable-frequency governor, directly carry out speed governing to motor, makes whirligig 5 reach predetermined number of revolutions.
Embodiment 1
Fig. 2 shows hand grenade instrumentation structural representation; According to the needs of lighter missile weight and shorter projection distance, the present invention proposes a kind of embodiment of rotating centrifugal transmitter of features simple structure, this embodiment is saved expensive motor and is controlled speed change gear, directly drive unit is substituted with rocking handle 6, with hand dynamic whirligig 5, according to test, also can by beyond the object emission of several kilograms extremely several kilometers, efficiency is also quite high.
Embodiment 2
Embodiment 2 shows a kind of electromagnetic release unit 7, Fig. 3 of the present invention and shows electromagnetic release device arrangement architecture; Fig. 4 is electromagnetic release device structural representation.Electromagnetic release unit 7, according to the arranged of launching tube 16, is arranged on the afterbody of each launching tube 16, utilizes wire 8 to be connected with control device 3 by each electromagnetic release unit 7.
Described electromagnetic release unit 7 comprises electromagnet, brute spring 12 and friction plate 9, wherein, the iron core 10 of electromagnet is hollow form, arrange coil 11 in iron core 10, the spatial placement brute spring 12 in the middle of iron core 10, brute spring 12 is stage clip, between electromagnet end cap 13 and electromagnet armature 14, the another side riveted joint friction plate 9 of armature 14; In normal conditions, electromagnet no power, under the effect of brute spring 12, friction plate 9 tightly pushes down emitting substance 4, makes emitting substance 4 be fixed in launching tube 16; When emission rate to be achieved and emission angle, control device 3 controls electromagnet conducting, produces electromagnetic attraction to armature 14, and friction plate 9 leaves the surface of emitting substance 4, and emitting substance 4 is launched in launching tube 16.
Operation principle of the present invention:
1, initial velocity V
0calculating (setting launching tube 16 is positioned at the edge of whirligig 5)
V
0＝Wx2x3.14xR
Wherein, W is whirligig 5 rotating speed per second, and R is the radius of whirligig 5.
2, as the substitute of firearms, the radius of setting whirligig 5 is 0.5 meter
Bullet goes out the initial velocity of bore generally at 300 meter per seconds
300 meter per seconds=W3.14
W=300/3.14 ≈ 96 revolutions per seconds of ≈ 5800 revolutions per seconds.
3, as the substitute of artillery, the radius of setting whirligig 5 is 2 meters, and shell goes out the highest 1900 meter per seconds of initial velocity of thorax
1900 meter per seconds=W6.28x2
W=1900/12.56 ≈ 150 revolutions per seconds of ≈ 9000 revolutions per seconds.
4, space-ward is launched an artificial satellite, need the first universal speed reached to be approximately 7800 meter per seconds
7800 meter per seconds=W6.28x2
W=7800/12.56 ≈ 620 revolutions per seconds of ≈ 37000 revolutions per seconds.
The radius strengthening whirligig 5 is 6 meters, then,
W=7800/37.68 ≈ 210 revolutions per seconds of ≈ 12400 revolutions per seconds.
In order to make whirligig 5 reach above-mentioned rotating speed, key is that the rotating speed of motor reaches requirement (or motor coordinate with speed change gear).
General alternating current generator is asynchronous machine, and that is, the rotating speed of rotor must be less than the rotating speed of rotating excitation field.General direct current generator is synchronous motor, and the rotating speed of rotor is synchronous with the change in magnetic field.The rotating speed of alternating current generator has maximum.The desirable maximum speed without the non-loaded motor of friction is also the rotating speed in infinite approach motor stator magnetic field.The number of poles of the rotating speed=a-c cycle/stator of rotating excitation field.The rotating speed of direct current generator can be infinitely great in theory, and in fact direct current generator is also the motor that rotating speed is the highest.
According to the formula n=60f/p of motor speed and frequency, the rotating speed (rev/min) of n-motor in above formula; F---supply frequency (He Zhi); The number of pole-pairs of p---electric machine rotary magnetic field.
Standard mains frequency is f=50 cycle per second, so the size of the rotating speed of rotating excitation field is only relevant with magnetic pole logarithm.Magnetic pole logarithm is many, and the rotating speed achievement of rotating excitation field is low.During number of pole-pairs P=1, the rotating speed n=3000 of rotating excitation field; During number of pole-pairs P=2, the rotating speed n=1500 of rotating excitation field; During number of pole-pairs P=3, the rotating speed n=1000 of rotating excitation field; During number of pole-pairs P=4, the rotating speed n=750 of rotating excitation field; During number of pole-pairs P=5, the rotating speed n=600 of rotating excitation field.
In frequency conversion speed-adjusting system, according to formula n=60f/p: change frequency f and just can change rotating speed, reduce frequency f, rotating speed just diminishes, and increases frequency f, and rotating speed just strengthens.
Generally centrifuge can be divided into following several pattern:
1, normal speed centrifuge rotating speed Fr≤3500 (being generally 600 ~ 1200), the rotating speed of this centrifuge is lower, and diameter is larger.
2, supercentrifuge Fr=3500 ~ 50000, the rotating speed of this centrifuge is higher, and general roller diameter is less, and length is longer.
3, Ultracentrifuge Fr > 50000, due to rotating speed very high (more than 50000r/min), so elongated tubular made by whirligig.
Select the centrifugal device of different size, above-mentioned data are that currently available technology can realize, and therefore, the present invention can as the replacement of conventional firearms, artillery and satellite launch.
Centrifugal quality grenade instrumentation of the present invention due to rotary body in High Rotation Speed can by the emitting substance being attached to rotary body edge tangentially high-speed projectile go out.Its kinetic energy determines according to the launch velocity degree at rotary body edge and emitting substance weight, and emission angle coordinates the distance of the object that determines to dish out; It is faster that rotary body turns, and the bullet of impelling is far away, and rotary body of the present invention is easy to bullet is transmitted into the first universal speed (7.8 kilometers/per second) this rank.Therefore the present invention can substitute cannon throws shells completely, and device can also be launched a guided missile after amplifying.Same emitter of the present invention can launch the bullet of different caliber, can single-shot, running fire or mass-sending, and this device volume is little lightweight, and disguised strong, launch accuracy is high.
Process described above is a kind of situation of the present invention; those skilled in the art and can require to augment without departing from the scope of the present invention calculating parameter, improve and change according to different targets, and above-mentioned supplement, improvement and replacing should all in the claims in the present invention protection domains.
Claims (7)
1. a rotating centrifugal transmitter, is characterized in that, described rotating centrifugal transmitter comprises: power set, control device, accelerator and base;
Described power set are made up of drive motors (1) and gear (15), and drive motors (1) adopts ac motor or the dc motor of different capacity and rotating speed;
Control device (3) adopts single-chip microcomputer or computer, controls the initial velocity of the transmitting of speed change gear (15) and emitting substance (4) and emission angle;
Described accelerator comprises whirligig (5), multiple launching tube (16) and electromagnetic release unit (7), described launching tube (16) is fixed on the edge of described whirligig (5) whole circumference, described whirligig (5) drives rotation to reach certain revolution by power set, makes the emitting substance (4) in launching tube (16) obtain certain initial velocity and kinetic energy;
Described base (2) supports whole device, providing stable and guide effect, improving fire accuracy for launching.
2. rotating centrifugal transmitter according to claim 1, is characterized in that, the length of described launching tube (16) is corresponding with the length of emitting substance (4), and launching tube arranges rifling in (16).
3. rotating centrifugal transmitter according to claim 2, is characterized in that, described speed change gear (15) adopts mechanical variable speed device or variable-frequency governor, makes whirligig (5) reach predetermined number of revolutions.
4. rotating centrifugal transmitter according to claim 3, is characterized in that, described mechanical variable speed device is speed-changing gear box.
5. rotating centrifugal transmitter according to claim 4, is characterized in that, described drive unit is rocking handle (6).
6. rotating centrifugal transmitter according to claim 5, it is characterized in that, described electromagnetic release unit (7) is according to the arranged of launching tube (16), be arranged on the afterbody of each launching tube (16), utilize wire (8) to be connected with control device (3) by each electromagnetic release unit (7).
7. rotating centrifugal transmitter according to claim 6, it is characterized in that, described electromagnetic release unit (7) comprises electromagnet, brute spring (12) and friction plate (9), wherein, the iron core (10) of electromagnet is hollow form, arranges coil (11) in described iron core (10); Spatial placement brute spring (12) in iron core (10), described brute spring (12) is stage clip, is positioned between electromagnet end cap (13) and electromagnet armature (14); Another side riveted joint friction plate (9) of described armature (14).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510522916.8A CN105115358A (en) | 2015-08-25 | 2015-08-25 | Rotational centrifugal launcher |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510522916.8A CN105115358A (en) | 2015-08-25 | 2015-08-25 | Rotational centrifugal launcher |
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| CN105115358A true CN105115358A (en) | 2015-12-02 |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107551434A (en) * | 2017-10-30 | 2018-01-09 | 宣士平 | Two generation fire fighting truck transmitters |
| CN108445078A (en) * | 2018-02-09 | 2018-08-24 | 深圳市睿灵创新科技开发有限公司 | Skin hollowing detection device and method |
| US10059472B2 (en) | 2016-04-19 | 2018-08-28 | SpinLaunch Inc. | Circular mass accelerator |
| CN108507405A (en) * | 2018-03-17 | 2018-09-07 | 宁波保税区攀峒信息科技有限公司 | One kind spinning up parabolic device and usage |
| CN109036026A (en) * | 2018-08-15 | 2018-12-18 | 诸葛佳缘 | A kind of physics hydraulic pressure interesting teaching demonstration equipment |
| CN109407176A (en) * | 2018-12-19 | 2019-03-01 | 华南农业大学 | A kind of ejection type three-dimensional space meteorologic parameter real-time measurement system and measurement method |
| CN109682951A (en) * | 2019-02-20 | 2019-04-26 | 中国水利水电科学研究院 | A kind of magnetic suspension centrifuge |
| WO2019164472A1 (en) * | 2018-02-20 | 2019-08-29 | SpinLaunch Inc. | Circular mass accelerator |
| CN110254754A (en) * | 2019-06-24 | 2019-09-20 | 北京机械设备研究所 | A kind of Space Rotating release device and rotation method for releasing |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10059472B2 (en) | 2016-04-19 | 2018-08-28 | SpinLaunch Inc. | Circular mass accelerator |
| US10202210B2 (en) | 2016-04-19 | 2019-02-12 | SpinLaunch Inc. | Circular mass accelerator |
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| CN108507405A (en) * | 2018-03-17 | 2018-09-07 | 宁波保税区攀峒信息科技有限公司 | One kind spinning up parabolic device and usage |
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| CN109407176A (en) * | 2018-12-19 | 2019-03-01 | 华南农业大学 | A kind of ejection type three-dimensional space meteorologic parameter real-time measurement system and measurement method |
| CN109407176B (en) * | 2018-12-19 | 2020-07-31 | 华南农业大学 | Ejection type three-dimensional space meteorological parameter real-time measurement system and measurement method |
| CN109682951A (en) * | 2019-02-20 | 2019-04-26 | 中国水利水电科学研究院 | A kind of magnetic suspension centrifuge |
| CN109682951B (en) * | 2019-02-20 | 2023-09-19 | 中国水利水电科学研究院 | Magnetic suspension centrifuge |
| CN110254754A (en) * | 2019-06-24 | 2019-09-20 | 北京机械设备研究所 | A kind of Space Rotating release device and rotation method for releasing |
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